US8522432B2ExpiredUtilityA1

Method of manufacturing a piston for a hydraulic motor having radial pistons

52
Assignee: LEMAIRE GILLESPriority: Mar 31, 2006Filed: Dec 8, 2011Granted: Sep 3, 2013
Est. expiryMar 31, 2026(expired)· nominal 20-yr term from priority
B23P 15/10Y10T29/49789Y10T29/49252F04B 1/0408Y10T29/49796Y10T29/49794Y10T29/4979F03C 1/0406Y10T29/49249Y10T29/49792Y10T29/49798
52
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Cited by
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References
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Claims

Abstract

A method for manufacturing radial pistons for a hydraulic motor by machining cylindrical transverse holes at regular intervals in a bar, and, in order to form two adjacent pistons, cutting up the bar on a transverse cutting-up plane passing through one of said holes so that a first portion of said hole forms a cradle-shaped recess in the base of the first one of the two adjacent pistons and so that another portion of said hole forms a cradle-shaped recess in the top of the second one of the two adjacent pistons.

Claims

exact text as granted — not AI-modified
The invention claimed is: 
     
       1. A method of manufacturing pistons for a hydraulic motor having radial pistons, each piston having a base, a top and a cradle-shaped recess, the method comprising the steps of:
 providing a cylindrical bar having a longitudinal axis, 
 machining cylindrical transverse through holes spaced apart uniformly in the bar, and 
 in order to form two adjacent pistons, cutting up the bar on a transverse cutting-up plane passing through one of said holes, so that a first portion of said hole forms a cradle-shaped recess having substantially the shape of a fraction of a cylinder in the base of the first one of the two adjacent pistons and so that another portion of said hole forms a cradle-shaped recess having substantially the shape of a fraction of a cylinder in a top of the second one of the two adjacent pistons. 
 
     
     
       2. A method according to  claim 1 , wherein the transverse cutting-up plane is offset relative to a transverse plane of symmetry of the hole through which said cutting-up plane passes so as to form the cradle-shaped recess in the base of the first one of the two adjacent pistons to be smaller than the cradle-shaped recess formed in the top of the second one of the two adjacent pistons. 
     
     
       3. A method according to  claim 1 , wherein additional machining operations, comprising at least one of rectification, treatment, de-burring, coating, lining, turning and milling are performed on the bar before the cutting step.

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